AD 91-16-02

Airworthiness directive · Shut-Off Valve Actuator · Airbus A320-111, A320-211, A320-212 and 4 more

Effective
September 11, 1991
Models
A320-111, A320-211, A320-212, A320-214, A320-231, A320-232, A320-233
Data sheet
TCDSA28NM
Registered aircraft
563 matched by model
Product
Aircraft · Large airplane
Amendment
39-7092
Docket
91-NM-59-AD

Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.

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The airworthiness directive

91-16-02 AIRBUS INDUSTRIE: Amendment 39-7092. Docket No. 91-NM-59-AD.

Applicability: Model A320 series airplanes, on which Modification 22039 has not been accomplished, certificated in any category.

Compliance: Required as indicated, unless previously accomplished.

To ensure complete closure of the low pressure fuel fire shut-off valve, accomplish the following:

A. Within 350 hours time-in-service after the effective date of this AD, and thereafter at intervals not to exceed 350 hours time-in-service, perform a functional check of the low pressure fuel fire shut-off valve actuator, in accordance with Airbus Industrie All Operators Telex (AOT) 28-01, dated October 8, 1990.

B. If any valve fails or indicates failure to open or close correctly, prior to further flight, replace the low pressure fuel fire shut-off valve actuator with either P/N HTE 190001 (PRE Airbus Industrie Service Bulletin A320-28-1028), or P/N HTE 190001-1 (POST Airbus Industrie ServiceBulletin A320-28-1028), in accordance with Airbus Industrie Service Bulletin A320-28-1028, Revision 1, dated November 23, 1990. Following actuator replacement, perform a functional test in accordance with AOT 28-01, dated October 8, 1990. Accomplishment of Modification 22039 (Service Bulletin A320-28-1028) constitutes terminating action for the repetitive functional checks required by paragraph A. of this AD.

C. An alternative method of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Standardization Branch, ANM-113, FAA, Transport Airplane Directorate.

NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector, who may concur or comment and then send it to the Manager, Standardization Branch, ANM-113.

D. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD.

E. The repetitive functional check requirements shall be done in accordance with Airbus Industrie All Operators Telex (AOT) 28-01, dated October 8, 1990. The replacement requirements shall be done in accordance with Airbus Industrie Service Bulletin A320-28-1028, Revision 1, dated November 23, 1990. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. Copies may be obtained from Airbus Industrie, Airbus Support Division, Avenue Didier Daurat, 31700 Blagnac, France. Copies may be inspected at the FAA, Transport Airplane Directorate, Renton, Washington; or at the Office of the Federal Register, 1100 L Street N.W., Room 8401, Washington, D.C.

This amendment (39-7092, AD 91-16-02) becomes effective on September 11, 1991.

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 563

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Airbus377 aircraft
  • Airbus Industrie184 aircraft
  • Airbus S A S2 aircraft
By year built
19912019
Registered aircraft by year built: 525 aircraft
19913
199213
19938
19941
19954
19967
19978
199825
199932
200035
200136
200225
200319
200418
200518
200625
200720
200820
200920
201017
201126
201232
201329
201419
201522
201614
201716
201811
20192

38 with no year recorded

By model

Aircraft

See all 563 aircraft